Performance of jet engine is dependent on the performance of compressor. This paper gives numerical study of performance characteristics for axial compressor. The test rig is present at CSIR LAB Bangalore. Flow domains are meshed and fluid dynamic equations are solved using ANSYS package. Analysis is done for six different speeds and for operating conditions like choke, maximum efficiency & before stall point. Different plots are compared and results are discussed. Shock displacement, vortex flows, leakage patterns are presented along with unsteady FFT plot and time step plot. © 2017 Author(s).
cited By ; Conference of International Conference on Functional Materials, Characterization, Solid State Physics, Power, Thermal and Combustion Energy 2017, FCSPTC 2017 ; Conference Date: 7 April 2017 Through 8 April 2017; Conference Code:129216
B. M. Prabhudev, S. Kumar, S., and Rajanna, D., “Numerical flow analysis of axial flow compressor for steady and unsteady flow cases”, in AIP Conference Proceedings, 2017, vol. 1859.